A constant-attitude landing system for STOL aircraft
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Authors
Craig, Andrew J.
Advisors
Issue Date
1960-01
Type
Thesis
Keywords
Citation
Abstract
Table of Contents
List of figures -- List of symbols -- Summary -- Introduction -- Development -- Conclusions -- References -- Appendix -- Description of the subject aircraft -- Development and solution of the aircraft -- Transfer functions -- Stability derivatives of the subject aircraft
Description
Thesis (M.S.)-- University of Wichita, College of Engineering, Dept. of Aeronautical Engineering
Publisher
Wichita State University

